N681QS
Service difficulty reports not matched to an aircraft · 19
They name N681QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N681QS' AND registry_match IS NULL ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N681QS' AND registry_match IS NULL ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DXTA2015062206035Light · intermittentRIGHT MLG GREEN DOWN & LOCKED LIGHT INTERMITTENT. RAN CHECKLISTS, GEAR WAS BLOWN DOWN HAD 3 GREEN LIGHTS ON LANDING.SDR DXTA2015051306016Control Cable · out of adjustIN STRAIGHT & LEVEL FLIGHT RUDDER TRIM REQUIRES 1/2 DEFLECTION TRIM TO LT. WITH FLAPS 35 & APPROACH AIRSPEED 3/4 DEFLECTION TO LT IS REQUIRED, REMOVED THE STINGER & INSTALLED BOTH THE RUDDER PEDAL BLOCKS & THE AFT SECTOR RIG PIN, WITH BOTH INSTALLED THE RUDDSDR DXTA2015051306017Unknown · unknownIN STRAIGHT & LEVEL FLIGHT RUDDER TRIM REQUIRES 1/2 DEFLECTION TRIM TO LT. WITH FLAPS 35 & APPROACH AIRSPEED 3/4 DEFLECTION TO LT IS REQUIRED.SDR DXTA2015022705987Actuator · malfunctionedTRIED TO MOVE THE RUDDER TRIM BOTH LT & RT. THE RUDDER TRIM WOULD NOT MOVE EITHER WAY. ON TAXI IN AFTER LANDING THE RUDDER PEDALS WERE STIFF TO STEER THE AIRPLANE. NO MECHANICAL DEFECTS WERE NOTED, HOWEVER THE RUDDER TRIM ACTUATOR DID NOT APPEAR TO HAVE MUCSDR DXTA2013052005398Bulb · burned outEXIT LIGHT OVER MAIN ENTRY DOOR WAS SEEN TO FLICKER ON AND OFF WHILE DECENDING FOR APPROACH. F/O NOTED A WISP OF SMOKE COMING FROM LIGHT. AFTER UNEVENTFUL LANDING AND DEPLANEING OF PASSENGERS, INSPECTED LIGHT AND FOUND ALL BULBS WERE OUT.SDR DXTR20130118003Bracket · crackedRUDDER AUTO/PILOT SERVO CABLE BRACKET IS CRACKED. R & R RUDDER AUTO/PILOT SERVO CABLE BRACKET IAW SRM 51-40-03.SDR DXTR20130118004Support · crackedRT WING TO FUSELAGE FAIRING ANGLE SUPPORT CRACKED IN SEVERAL SPOTS. R & R RT AFT STRAP (PN 6610146-20-1) IAW SRM 51-40-03.SDR DXTA2011082904712Apu · leaking5 MINUTES AFTER ENGINE START, GRAY SMOKE BEGAN FILLING CABIN. APU HAD BEEN RUNNING FLAWLESSLY FOR 40 MINUTES. PERFORMED VISUAL INSP OF THE APU INLET, FOUND OIL RESIDUE IN THE APU INTAKE. REMOVE EXCHANGE NOZZLE, INLET AIR DUCT, CONNECTORS, FUEL AND DRAIN LINESDR DXTA2011030304489Bearing · wornVIBRATION IN AIRFRAME. MOST NOTABLE AT HIGHER SPEEDS-290K. NOT NOTICEABLE AT SPEEDS LESS THAN 240K. NO CHANGES WITH CONFIGURATION CHANGE. VIBRATION FELT THROUGHOUT AIRFRAME, AUTOPILOT ON AND OFF. R & R ELEVATOR, LT TRIM TAB HORN BEARINGS AND REPLACED RUDDSDR DXTA2010092004245Ahrs · failedDURING FTL LT PFD AND MFD DISPLAYED ATTITUDE AND HEADING FAILED. TROUBLESHOT AND FOUND NR 1 AHRS TO BE INOPERATIVE. R & R NR1 AHRS UNIT REPAIRED IAW MM 34-21-01. OPS CHECKED GOOD.SDR DXTA200810213313Actuator · inoperativeAT 400 FT AND SELECTING FLAPS FROM 15 TO ZERO DEGREES, HYD PRESS ANNUNCIATOR AND MASTER CAUTION BEGAN FLASHING AND FLAPS INDICATOR STOPPED AT 7 DEGREES. IAW AA2 CB WAS PULLED AND LIGHTS EXTINGUISHED. RESET CB FOR LDG AND LT FLAPS A 7 DEGREES FOR LDG AND POST FSDR DXTA2008102203313Flap System · malfunctionedAT 400FT AND SELECTING FLAPS FROM 15 TO ZERO DEGREES, FLAPS INDICATOR STOPPED AT 7 DEGREES.SDR DXTA200808263249Actuator · obstructedAFTER TAKEOFF, FLAPS STOCK AT 7 (DEG) WITH ACCOMPANYING MASTER CAUTION AND HYD PRESS ANNUNCIATIONS. CAUTION CEASED WHEN FLAPS SELECTED 15 (DEG) AND GEAR DOWN. VERIFIED DISCREPANCY TROUBLESHOT TO FAULTY LT FLAP ACTUATOR. GAINED ACCESS TO LT FLAP ACTUATOR AND RSDR DXTA200702629Warning Light · illuminatedFLAP OVERSPEED ON DEPARTURE CLIMB. COMPLIED WITH FLAP OVERSPEED INSPECTION IAW MM 5-50-00 NO DEFECTS NOTED.SDR DXTA200702467Windshield · failedPIC SIDE WINDSHIELD SHATTERED AT FL430. REMOVED AND INSTALLED A NEW WINDSHIELD IN THE PILOTS POSITION. INSTALLED WITH NEW HARDWARE- TORQUED PER M/M. INSTALLED WITH NEW STICK N STRIP SEAL. PRESSURIZED AIRCRAFT. LEAK RATE WITHIN LIMITS. RAN A/C TO OPS CHECK PSDR DXTA200702170Connector · corrodedDURING TAKEOFF ROLL, ABORTED TAKEOFF (BELOW 70KTS) DUE TO ILLUMINATION OF NO TAKEOFF ANNUNCIATOR AND NO TAKEOFF HORN. TROUBLESHOT SYSTEMS. FOUND EXCESSIVE MOISTURE AND CORROSION IN THE LT SPEEDBRAKE DISCONNECT PLUG PL001. REPLACED PINS, SOCKETS AND PLUG BACSDR DXTA200501025Warning Light · illuminatedON TAKEOFF WHEN GEAR WAS RETRACTED GEAR UNLOCK LIGHT & HYD PUMP ANNUNCIATOR LIGHT REMAINED ILLUMINATED. GEAR WAS CYCLED DOWN WITH LOCK INDICATION HYD PUMP EXTINGUISHED. ITEM IS UNDER INVESTIGATION.SDR DXTA200300179Coalescer Bag · dirtyAFTER TAKEOFF FROM LNK, NOTICE BURNING ODOR IN COCKPIT WITH POWER AT OR ABOVE 70 PERCENT AND APU OFF, ACCOMPLISHED AIR TURNBACK TO LNK. INVESTIGATED AND FOUND WATER SOCK AREA CLEAN AND FREE OF ODOR PER CESSNA 560XL MM CHAPTER 21-50-00, SYSTEM OPS CHECKED OK.SDR DXTA200300175Acm · odorAFTER TAKE OFF AN ACRID SMELL WAS DETECTED IN COCKPIT. THIS WAS FOLLOWED BY A BURNING IN THE THROATS AND EYES OF PASSENGERS AND CREW. DECLARED AN EMERGENCY, O2 GEAR WAS DONNED AND RETURNED TO KLNK. NO SMOKE WAS EVER VISIBLE. TROUBLESHOT TO FIND SOURCE FOR
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